# STC SR02139SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Onboard Systems International, United States - Description: Fabrication of Onboard Systems Model 200-355-00 and 200-369-00 Cargo Hook Fixed Provision Kits, Model 200-356-00 Cargo Hook Suspension Kit, and Model 200-357-00 Load Weigh Kit, in accordance with FAA Approved Onboard Systems Master Drawing List No. 155-160-00, Revision 2, dated September 27, 2011, or later FAA approved revision. Installation of the Onboard Systems Model 200-355-00, 200-356-00, 200-357-00, or 200-369-00 kits in accordance with FAA approved Onboard Systems Owners Manual 120-141-00, Revision 0, dated April 25, 2011, or later FAA approved revision. This modification must be inspected and maintained in accordance with section ATA 5 of FAA approved Onboard Systems Instructions for Continued Airworthiness Document 123-036-00, Revision 0, dated May 5, 2011, or later FAA approved revision, and Onboard Systems Cargo Hook - Applied: September 17, 2009 - Status date: October 4, 2011 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H7EU](https://openairdocs.org/tcds/H7EU) - Certificate PDF: https://openairdocs.org/files/sha256/04/f2/04f2c654e8315d20fd681c40b43073774539c68b67e5b01df7c1394da2bc48be - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D189740AB73C365B8625793C0070F998.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR02139SE ## ADs that name it (0) None. ## Approved models (3) - Agusta S.p.A. A109E ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. A119 ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) - Agusta S.p.A. AW119 MKII ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SR02139SE This certificate issued to: Onboard Systems 13915 NW 3 rd Court Vancouver, WA 98685 Part 27 of the Federal Aviation Regulations Original ProductType Certificate Number: H7EU Make: Agusta S.p.A Model: A109E/A119/AW119 MK II Description of the Type Design Change: Fabrication of Onboard Systems Model 200-355-00 and 200-369-00 Cargo Hook Fixed Provision Kits, Model 200-356-00 Cargo Hook Suspension Kit, and Model 200-357-00 Load Weigh Kit, in accordance with FAA Approved Onboard Systems Master Drawing List No. 155-160-00, Revision 2, dated September 27, 2011, or later FAA approved revision. Installation of the Onboard Systems Model 200-355- 00, 200-356-00, 200-357-00, or 200-369-00 kits in accordance with FAA approved Onboard Systems Owners Manual 120-141-00, Revision 0, dated April 25, 2011, or later FAA approved revision. This modification must be inspected and maintained in accordance with section ATA 5 of FAA approved Onboard Systems Instructions for Continued Airworthiness Document 123-036-00, Revision 0, dated May 5, 2011, or later FAA approved revision, and Onboard Systems Cargo Hook Service Manual 122-015-00, Revision 12, dated October 25, 2010, or later FAA approved revision. Limitations and Conditions: Approval of this change in type design applies to only those model rotorcraft listed above. This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft. Rotorcraft modified in accordance with this STC must be operated in accordance with a copy of FAA approved Onboard Systems Rotorcraft Flight Manual Supplement (RFMS) No. 121-055-00, Revision 0, dated July 8, 2011, or later FAA approved revision. A copy of this Certificate, the FAA approved RFMS, and maintenance manuals must be maintained as a part of the permanent records of the modified rotorcraft. Date of application: September 17, 2009 Date reissued: October 4, 2011 Date of issuance: September 13, 2011 Date amended: Any alteration of this certificat e is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2(10-68 By direction of the Administrator (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (2) - October 4, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/04/f2/04f2c654e8315d20fd681c40b43073774539c68b67e5b01df7c1394da2bc48be) - September 13, 2011: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/21/77/21771878d41100902e0d9889142ca43ca7799e56f870dae355e199f5c8546742) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.